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1Formulas and methods
Series & parallel resistors
Resistors in series
Req = R1 + R2 + …
Resistors in parallel
1/Req = 1/R1 + 1/R2 + …
Two in parallel
Req = R1R2 / (R1 + R2)
Ohm's law
V = I·R
Power
P = V·I = I²R = V²/R
Method
Start at the end of the network furthest from the terminals.
Combine resistors in series by adding them, and resistors in parallel with 1/R = 1/R₁ + 1/R₂ + …
Redraw the circuit after each step.
Repeat until one resistor is left between the terminals.
Nodal analysis
Kirchhoff’s current law
ΣIin = ΣIout
Branch current
I = (Va − Vb)/R
Reference node
Vground = 0
Method
Choose a reference node (ground) and label the other node voltages.
Write Kirchhoff’s current law at every unknown node: currents leaving through each branch equal the currents entering.
Express every branch current as (Va − Vb)/R.
Solve the system of equations, then find any current you need.
Mesh analysis
Kirchhoff’s voltage law
ΣV = 0 around every loop
Shared resistor
current = I1 − I2
Current source in a mesh
fixes that mesh current
Method
Draw a clockwise current in every mesh (window) of the circuit.
Apply Kirchhoff’s voltage law around each mesh: the sum of voltage drops is zero.
In a resistor shared by two meshes the current is the difference of the two mesh currents.
Solve the equations; a negative result means the current flows the other way.
Superposition
Superposition
x = x1 + x2 + … (one source at a time)
Switched-off voltage source
short circuit (0 V)
Switched-off current source
open circuit (0 A)
Voltage divider
V2 = V·R2/(R1 + R2)
Current divider
I1 = I·R2/(R1 + R2)
Method
Count the independent sources. You will solve one simpler circuit per source.
Keep one source and switch off the others: a voltage source becomes a short circuit (a wire), a current source becomes an open circuit (a gap).
Solve the simpler circuit for the voltage or current you need, keeping track of its direction.
Repeat for every source, then add the contributions with their signs.
Thévenin & Norton
Thévenin voltage
Vth = Vopen circuit
Thévenin resistance
Rth: all sources off, seen from a–b
Norton current
IN = Vth/Rth
Load current
IL = Vth/(Rth + RL)
Maximum power transfer
RL = Rth, Pmax = Vth²/(4Rth)
Method
Remove the load and mark the two terminals a and b.
Find the open-circuit voltage between a and b: this is Vth.
Switch off all independent sources and find the resistance seen from a–b: this is Rth.
Put the load back on the equivalent circuit: Vth in series with Rth.
For the Norton equivalent, convert: IN = Vth/Rth, with RN = Rth in parallel.
RC & RL transients
Time constant
τ = RC | τ = L/R
Response
x(t) = x(∞) + [x(0) − x(∞)]·e−t/τ
Capacitor at DC
open circuit; vC cannot jump
Inductor at DC
short circuit; iL cannot jump
Settled
t ≈ 5τ
Method
Find the initial value just after switching: a capacitor voltage and an inductor current cannot jump.
Find the final value long after switching: a capacitor acts as an open circuit, an inductor as a short circuit.
Find the time constant: τ = RC or τ = L/R, using the resistance seen by the capacitor or inductor.
Use x(t) = x(∞) + [x(0) − x(∞)]·e−t/τ.
AC impedance & phasors
Impedances
ZR = R, ZL = jωL, ZC = 1/(jωC)
Angular frequency
ω = 2πf
Magnitude and angle
|Z| = √(R² + X²), φ = atan(X/R)
Phasor Ohm’s law
V = I·Z
Method
Convert the frequency: ω = 2πf.
Find each reactance: XL = ωL and XC = 1/(ωC).
Add impedances like resistors, with Z = R + jX.
Find the magnitude |Z| = √(R² + X²) and the angle φ = atan(X/R), then use Ohm’s law with phasors.
AC power & power factor
Real power
P = V·I·cos φ
Reactive power
Q = V·I·sin φ
Apparent power
S = V·I = √(P² + Q²)
Power factor
pf = cos φ = P/S
Correction capacitor
QC = P(tan φ1 − tan φ2), C = QC/(ωV²)
Three-phase power
Y connection
VL = √3·Vph, IL = Iph
Δ connection
VL = Vph, IL = √3·Iph
Total real power
P = √3·VL·IL·cos φ = 3·Iph²·R
Apparent and reactive power
S = √3·VL·IL, Q = P·tan φ
Correction capacitors
QC = P(tan φ1 − tan φ2), C = QC/(3ωV²)
Voltage across each capacitor
Δ: VL Y: VL/√3
Motor input
Pin = Pout/η
Transformers
Turns ratio
a = N1/N2 = V1/V2
Current ratio
I1/I2 = N2/N1 = 1/a
Rated current
I = S/V
Referred impedance
Z1′ = a²·ZL
Copper loss at part load
Pcu = x²·Pcu,fl
Efficiency
η = x·S·pf/(x·S·pf + Pcore + x²·Pcu,fl)
Maximum efficiency
x = √(Pcore/Pcu,fl)
Op-amp circuits
Inverting amplifier
Vout = −(Rf/Rin)·Vin
Non-inverting amplifier
Vout = (1 + Rf/R1)·Vin
Summing amplifier
Vout = −Rf(V1/R1 + V2/R2)
Ideal op-amp
V+ = V−, Iin = 0
Diodes & transistors
Diode (constant drop)
VD = 0.7 V when conducting
Active region
VBE = 0.7 V, IC = β·IB, IE = (β + 1)·IB
Fixed bias
IB = (VCC − 0.7)/RB
Divider bias
IB = (VTH − 0.7)/(RTH + (β + 1)RE)
Thévenin of the divider
VTH = VCC·R2/(R1 + R2), RTH = R1∥R2
Collector loop
VCE = VCC − ICRC − IERE
Saturation
IC(sat) = (VCC − VCE(sat))/RC, IB ≥ IC(sat)/β
Number systems
Place values
binary 2k, octal 8k, hex 16k
To decimal
Σ dk·bk
From decimal
divide by the base, read the remainders bottom-up
Hex ↔ binary
one hex digit = 4 bits
Two’s complement
invert the bits and add 1
Digital logic: gates, K-maps & flip-flops
Basic gates
A·B, A + B, A′, (A·B)′, (A + B)′, A ⊕ B
Boolean rules
X + X′ = 1, X·X′ = 0, X + XY = X, XY + XY′ = X
De Morgan
(X·Y)′ = X′ + Y′, (X + Y)′ = X′·Y′
Karnaugh map order
00, 01, 11, 10 (Gray code)
Group of 2ᵏ cells
loses k variables
4-to-1 multiplexer
F = A′B′I0 + A′BI1 + AB′I2 + ABI3
Flip-flops
D: Q⁺ = D, T: Q⁺ = T ⊕ Q, JK: Q⁺ = JQ′ + K′Q
Counters
n-bit: 2ⁿ states; mod-N: smallest n with 2ⁿ ≥ N; fout = fclk/N
Ripple counter
fmax = 1/(n·tpd)
Ring and Johnson counters
n and 2n states
Method
For a circuit, work from the inputs to the output one gate at a time and write the value on every wire, or write its expression and fill in the truth table.
For simplification, put the 1s (and the don’t-cares as X) into a Karnaugh map with Gray-code rows and columns: 00, 01, 11, 10.
Cover the 1s with as few and as large groups of 1, 2, 4, 8 or 16 cells as possible, wrapping round the edges; each group is one product term made of the variables that stay constant. Group the 0s for the POS form.
For flip-flops and counters, read the inputs at each active clock edge, write the state after every edge, and remember that an n-bit counter wraps round after 2ⁿ states.
Stability: Routh–Hurwitz & root locus
Stability
all roots of the characteristic polynomial in the left half-plane
Routh array, s¹ entry of a cubic
b1 = (a2a1 − a3a0)/a2
Right half-plane roots
number of sign changes in the first column
Cubic s³ + a₂s² + a₁s + a₀
stable when all a > 0 and a₂·a₁ > a₀
K/(s(s + a)(s + b))
Kmax = ab(a + b), ω = √(ab)
Characteristic equation
1 + K·G(s) = 0
Asymptotes
σa = (Σp − Σz)/(n − m), θ = (2q + 1)·180°/(n − m)
Break-away and break-in points
dK/ds = 0
Magnitude condition
K = 1/|G(s)|
Angle of departure
θd = 180° − Σ∠(from other poles) + Σ∠(from zeros)
Method
Write the closed-loop characteristic polynomial: the denominator of 1 + K·G(s) = 0, multiplied out.
Put the coefficients alternately into the first two rows of the Routh array and build the remaining rows.
Count the sign changes in the first column: each one is a pole in the right half-plane. With K in the array, demand that every first-column entry stays positive.
For a root locus, mark the poles and zeros, the real-axis segments, the asymptotes from the centroid and the break points where dK/ds = 0. Use K = 1/|G(s)| for the gain at a point.
Steady-state error & PID control
System type
number of poles of G(s) at s = 0
Error constants
Kp = lim G(s), Kv = lim s·G(s), Ka = lim s²·G(s) (s → 0)
Step A
ess = A/(1 + Kp)
Ramp A·t
ess = A/Kv
Parabola A·t²/2
ess = A/Ka
PID controller
C(s) = Kp + Ki/s + Kd·s
Second-order target
s² + 2ζωns + ωn²
Overshoot and timing
%OS = 100·e−ζπ/√(1−ζ²), tp = π/ωd, ts ≈ 4/(ζωn)
Method
Count the poles of the open loop C(s)·G(s) at s = 0: that is the system type.
Work out the error constant that matches the input: Kp for a step, Kv for a ramp, Ka for a parabola.
Apply ess = A/(1 + Kp), A/Kv or A/Ka, or solve it for the gain you need.
For a damping or speed specification, write the closed-loop characteristic polynomial and match it with s² + 2ζω_n·s + ω_n².
2Practice problems
1.Series & parallel resistorsMedium
Find the equivalent resistance Req seen by the source V1.
V1 = 12 VR1 = 20 ΩR2 = 5 ΩR3 = 2 ΩR4 = 10 Ω
Req = Ω
2.Series & parallel resistorsHard
Find the equivalent resistance Req seen by the source V1.
Find the Thévenin resistance Rth seen from terminals a–b.
V1 = 18 VR1 = 12 ΩR2 = 2 ΩR3 = 5 Ω
Rth = Ω
10.Thévenin & NortonHard
Find the Norton current IN: the current that flows from a to b if the terminals are shorted.
V1 = 18 VIs = 4 AR1 = 2 ΩR2 = 6 ΩR3 = 3 Ω
IN = A
11.RC & RL transientsMedium
The inductor carries a steady current of 2 A. At t = 0 the switch closes the loop through R and the source is removed, so the inductor current decays through R. How long does it take for the current to fall to 0.4 A? Find t.
i(0) = 2 AR = 15 ΩL = 150 mH
t = ms
12.RC & RL transientsHard
The switch across R2 has been open for a long time, so the inductor current is steady. At t = 0 the switch closes and shorts out R2. Find the inductor current i at t = 20 ms.
Vs = 20 VR1 = 20 ΩR2 = 10 ΩL = 220 mHt = 20 ms
i = A
13.AC impedance & phasorsMedium
A series RLC circuit is connected to a 24 V (rms), 60 Hz supply. Find the rms current I.
V = 24 V (rms)f = 60 HzR = 20 ΩL = 50 mHC = 47 µF
I = A
14.AC impedance & phasorsHard
A resistor R1 is connected in series with a parallel combination of R2 and a capacitor C, across a 120 V (rms), 60 Hz supply. Find the rms current I.
V = 120 V (rms)f = 60 HzR1 = 15 ΩR2 = 20 ΩC = 100 µF
I = A
15.AC power & power factorMedium
A load with impedance Z = 12 + j9 Ω is connected to a 120 V (rms) single-phase supply. Find the reactive power Q it absorbs.
V = 120 VZ = 12 + j9 Ω
Q = var
16.AC power & power factorHard
A single-phase load takes 29 kW at a power factor of 0.75 lagging from a 240 V, 50 Hz supply. A 330 µF capacitor is connected in parallel with the load. Find the new line current I.
P = 29 kWpf1 = 0.75V = 240 Vf = 50 HzC = 330 µF
I = A
17.Three-phase powerMedium
A three-phase induction motor delivers 55 kW of mechanical output power at full load. At this load its efficiency is 94% and its power factor is 0.82 lagging. The supply has a line-to-line voltage of 690 V. Find the line current IL.
Pout = 55 kWη = 94%cos φ = 0.82VL = 690 V
IL = A
18.Three-phase powerHard
A balanced three-phase load takes 300 kW at a power factor of 0.75 lagging from a 690 V (line-to-line), 60 Hz supply. A three-phase capacitor bank in parallel with the load must raise the overall power factor to 0.98 lagging. The real power stays the same. Find the total reactive power QC the capacitor bank must supply, in kvar.
P = 300 kWpf1 = 0.75pf2 = 0.98VL = 690 Vf = 60 Hz
QC = kvar
19.TransformersMedium
A 4 Ω resistor is connected across the secondary winding of an ideal transformer with a turns ratio N₁:N₂ = 12:1. Find the resistance R1′ seen looking into the primary winding.
N1:N2 = 12:1RL = 4 Ω
R1′ = Ω
20.TransformersHard
A single-phase 50 kVA transformer has a core loss of 400 W. At rated load and a power factor of 0.95 lagging its efficiency is 97.5%. Find the full-load copper loss Pcu,fl in watts.
S = 50 kVAPcore = 400 Wpf = 0.95η = 97.5%
Pcu,fl = W
21.Op-amp circuitsMedium
Choose the feedback resistor Rf that gives this non-inverting amplifier a voltage gain of 51.
R1 = 4.7 kΩAv = 51
Rf = kΩ
22.Op-amp circuitsHard
Two ideal op-amp stages are connected in cascade: an inverting amplifier (R1, Rf1) followed by a non-inverting amplifier (R2 to ground, Rf2 in the feedback). Both run from ±15 V supplies. The input is Vin = 0.3 V. Find the output voltage Vout.
A 5.1 V Zener regulator is fed from 18 V through 680 Ω and supplies a 3300 Ω load. Find the Zener current IZ.
Vin = 18 VVZ = 5.1 VR = 680 ΩRL = 3300 Ω
IZ = mA
24.Diodes & transistorsHard
A 5.1 V Zener regulator has a 470 Ω series resistor. The input can rise to 16 V, and the load may be disconnected. Find the largest power PZ,max the Zener must dissipate.
Vin,max = 16 VVZ = 5.1 VR = 470 Ω
PZ,max = mW
25.Number systemsMedium
The 8-bit pattern 0111 1001 stores a signed integer in two's complement. What is its value N in decimal?
0111 10018 bit
N =
26.Number systemsHard
An uncompressed image is 1280 × 720 pixels with 32 bits per pixel. How much memory M does it take, in KiB (1 KiB = 1024 bytes)?
In this Karnaugh map exactly one 1 has no neighbouring 1, so it stays a group of one cell (a full minterm of four literals) in the minimal SOP form. Neighbours across the map edges count. Click that cell.
F = Σm(1, 4, 9, 10, 14)
1AB = 00, CD = 00
2AB = 00, CD = 01
3AB = 00, CD = 11
4AB = 00, CD = 10
5AB = 01, CD = 00
6AB = 01, CD = 01
7AB = 01, CD = 11
8AB = 01, CD = 10
9AB = 11, CD = 00
10AB = 11, CD = 01
11AB = 11, CD = 11
12AB = 11, CD = 10
13AB = 10, CD = 00
14AB = 10, CD = 01
15AB = 10, CD = 11
16AB = 10, CD = 10
28.Digital logic: gates, K-maps & flip-flopsHard
A 20 kHz clock drives a mod-50 counter. Find the frequency fout of its most significant output, which completes one cycle per counting cycle.
fclk = 20 kHzN = 50
fout = kHz
29.Laplace transformsMedium
Find f(t) for F(s) = (4s + 6)/(s² + 6s + 9) and evaluate f(0.3).
F(s) = (4s + 6)/(s² + 6s + 9)t = 0.3 s
f(0.3) =
30.Laplace transformsHard
A system is described by the differential equation y″ + 6y′ + 8y = 3u′ + 16u, with input u(t) and output y(t). Find its transfer function G(s) = Y(s)/U(s) (zero initial conditions) and evaluate the impulse response g(t) at t = 0.5 s. Find g(0.5).
y″ + 6y′ + 8y = 3u′ + 16ut = 0.5 s
g(0.5) =
31.Block diagramsMedium
A plant G(s) = 30/(s + 6) is controlled in a negative feedback loop whose sensor has the gain H = 0.5. A step of size 10 is applied at R. Find the steady-state output css.
G(s) = 30/(s + 6)H = 0.5R = 10
css =
32.Block diagramsHard
The plant G(s) = K/(s(s + 2)(s + 6)) is in a unity negative feedback loop. At the largest stable gain the loop oscillates. Find the frequency of oscillation ω in rad/s.
G(s) = K/(s(s + 2)(s + 6))unity negative feedback
ω = rad/s
33.Step responseMedium
A system has the transfer function G(s) = 15/(s² + 7s + 30) and receives a unit step input. Find the 2 % settling time ts of the step response, using ts ≈ 4/(ζωₙ).
G(s) = 15/(s² + 7s + 30)
ts = s
34.Step responseHard
A unity negative feedback loop has G(s) = K/(s(s + 5)). Find the gain K that gives a step response with 10 % overshoot.
G(s) = K/(s(s + 5))%OS = 10 %
K =
35.Bode plots & marginsMedium
The RL high-pass filter shown has R = 10 Ω, L = 100 mH. A sinusoidal input of 8 Hz is applied. Find the phase shift φ of vout relative to vin, in degrees.
R = 10 ΩL = 100 mHf = 8 Hz
φ = °
36.Bode plots & marginsHard
A unity-feedback loop has the open-loop transfer function L(s) = 23/(s(s + 10)). Find the gain crossover frequency ωc, where |L(jω)| = 1.
L(s) = 23/(s(s + 10))
ωc = rad/s
37.Stability: Routh–Hurwitz & root locusMedium
The loop in the diagram has negative feedback and L(s) = 40/(s(s + 1)(s + 4)). How many closed-loop poles N lie in the right half-plane?
L(s) = 40/(s(s + 1)(s + 4))
N =
38.Stability: Routh–Hurwitz & root locusHard
A unity-feedback loop has L(s) = K(s + 3)/(s(s + 2)(s + 6)). Find the point σa where the asymptotes of the root locus cross the real axis.
L(s) = K(s + 3)/(s(s + 2)(s + 6))
σa =
39.Steady-state error & PID controlMedium
A ramp r(t) = 0.5t is applied to a unity-feedback loop with G(s) = 2/(s(s + 5)(s + 10)). Find the steady-state error ess.
G(s) = 2/(s(s + 5)(s + 10))r(t) = 0.5t
ess =
40.Steady-state error & PID controlHard
A proportional controller K = 2 drives the plant G(s) = 4/(s(s + 2)) in a unity-feedback loop. Find the 2 % settling time ts of the step response, using ts ≈ 4/(ζωₙ).
G(s) = 4/(s(s + 2))K = 2
ts = s
3Solutions
1.Series & parallel resistors
Answer: Req = 23.53 Ω
Series and parallel resistors: in series the same current flows through each resistor and R = R₁ + R₂ + …. In parallel each resistor has the same voltage and 1/R = 1/R₁ + 1/R₂ + …. A ladder network is reduced one pair at a time until a single equivalent resistance remains.
Combine resistors from the far end
Start at the end farthest from the source and work back towards it. Resistors carrying the same current are in series; resistors across the same two nodes are in parallel.
R3 + R4 = 2 + 10 = 12 Ω
R2 ∥ 12 = 5·12/(5+12) = 3.529 Ω
Req = R1 + 3.529 = 20 + 3.529 = 23.53 Ω
Answer
Req = 23.53 Ω
2.Series & parallel resistors
Answer: Req = 14.37 Ω
Series and parallel resistors: in series the same current flows through each resistor and R = R₁ + R₂ + …. In parallel each resistor has the same voltage and 1/R = 1/R₁ + 1/R₂ + …. A ladder network is reduced one pair at a time until a single equivalent resistance remains.
Combine resistors from the far end
Start at the end farthest from the source and work back towards it. Resistors carrying the same current are in series; resistors across the same two nodes are in parallel.
R5 + R6 = 10 + 8 = 18 Ω
R4 ∥ 18 = 3.273 Ω
R3 + 3.273 = 11.27 Ω
R2 ∥ 11.27 = 2.369 Ω
Req = R1 + 2.369 = 12 + 2.369 = 14.37 Ω
Answer
Req = 14.37 Ω
3.Nodal analysis
Answer: IR3 = 0.4615 A
Nodal analysis: choose a reference node, label the unknown node voltages, write Kirchhoff’s current law at each unknown node using Ohm’s law (I = ΔV/R), and solve the resulting equations.
Set up the nodes
Ground is the bottom wire. Known node voltages come straight from the sources (V1 = 24 V). Unknowns: VA, VB.
KCL at node A
Currents leaving A through the resistors equal the current pushed into A by sources.
VA/R2 + (VA − V1)/R1 + (VA − VB)/R3 = 0
VA/12 + (VA − 24)/4 + (VA − VB)/2 = 0
0.8333·VA − 0.5·VB = 6
KCL at node B
Currents leaving B through the resistors equal the current pushed into B by sources.
VB/R4 + (VB − VA)/R3 = Is
VB/8 + (VB − VA)/2 = 1.5
−0.5·VA + 0.625·VB = 1.5
Solve
Δ = (0.8333)(0.625) − (−0.5)(−0.5) = 0.2708
VA = Δ1/Δ = 4.5/0.2708 = 16.62 V
VB = Δ2/Δ = 4.25/0.2708 = 15.69 V
Answer
IR3 = (VA − VB)/R3 = (16.62 − 15.69)/2 = 0.4615 A
4.Nodal analysis
Answer: IR4 = −0.5701 A
Nodal analysis: choose a reference node, label the unknown node voltages, write Kirchhoff’s current law at each unknown node using Ohm’s law (I = ΔV/R), and solve the resulting equations.
Set up the nodes
Ground is the bottom wire. Known node voltages come straight from the sources (V1 = 36 V, V2 = 36 V). Unknowns: VA, VB.
KCL at node A
Currents leaving A through the resistors equal the current pushed into A by sources.
VA/R3 + (VA − V1)/R1 + (VA − VB)/R2 = 0
VA/2 + (VA − 36)/4 + (VA − VB)/8 = 0
0.875·VA − 0.125·VB = 9
KCL at node B
Currents leaving B through the resistors equal the current pushed into B by sources.
VB/R5 + (VB − VA)/R2 + (VB − V2)/R4 = Is
VB/30 + (VB − VA)/8 + (VB − 36)/15 = 2
−0.125·VA + 0.225·VB = 4.4
Solve
Δ = (0.875)(0.225) − (−0.125)(−0.125) = 0.1812
VA = Δ1/Δ = 2.575/0.1812 = 14.21 V
VB = Δ2/Δ = 4.975/0.1812 = 27.45 V
Answer
IR4 = (VB − V2)/R4 = (27.45 − 36)/15 = −0.5701 A
5.Mesh analysis
Answer: VR2 = −7.941 V
Mesh analysis: give each window of a planar circuit its own loop current, write Kirchhoff’s voltage law around each loop (sum of drops = sum of rises), and solve. Branch currents are the mesh current, or the difference of two mesh currents on a shared branch.
Assign mesh currents
Draw a clockwise current in each window: I1, I2. A resistor shared by two meshes carries the difference of their currents.
KVL around mesh 1
Going clockwise, the voltage drops across resistors equal the source voltage rises (− to + in the direction of travel).
R1·I1 + R3(I1 − I2) = V1
8·I1 + 20(I1 − I2) = 15
28·I1 − 20·I2 = 15
KVL around mesh 2
Going clockwise, the voltage drops across resistors equal the source voltage rises (− to + in the direction of travel).
R2·I2 + R3(I2 − I1) = −V2
4·I2 + 20(I2 − I1) = (−30)
−20·I1 + 24·I2 = −30
Solve
Δ = (28)(24) − (−20)(−20) = 272
I1 = Δ1/Δ = −240/272 = −0.8824 A
I2 = Δ2/Δ = −540/272 = −1.985 A
Answer
IR2 = I2 = −1.985 A
VR2 = IR2·R2 = −1.985·4 = −7.941 V
A negative mesh current flows anticlockwise.
6.Mesh analysis
Answer: VR5 = 5.574 V
Mesh analysis: give each window of a planar circuit its own loop current, write Kirchhoff’s voltage law around each loop (sum of drops = sum of rises), and solve. Branch currents are the mesh current, or the difference of two mesh currents on a shared branch.
Assign mesh currents
Draw a clockwise current in each window: I1, I2, I3. A resistor shared by two meshes carries the difference of their currents.
KVL around mesh 1
Going clockwise, the voltage drops across resistors equal the source voltage rises (− to + in the direction of travel).
R1·I1 + R4(I1 − I2) = V1
20·I1 + 12(I1 − I2) = 6
32·I1 − 12·I2 = 6
KVL around mesh 2
Going clockwise, the voltage drops across resistors equal the source voltage rises (− to + in the direction of travel).
R2·I2 + R4(I2 − I1) + R5(I2 − I3) = 0
5·I2 + 12(I2 − I1) + 2(I2 − I3) = 0
−12·I1 + 19·I2 − 2·I3 = 0
KVL around mesh 3
Going clockwise, the voltage drops across resistors equal the source voltage rises (− to + in the direction of travel).
R3·I3 + R5(I3 − I2) = −V2
8·I3 + 2(I3 − I2) = (−30)
−2·I2 + 10·I3 = −30
Solve
Δ = det of the coefficient matrix = 4512
I1 = Δ1/Δ = 396/4512 = 0.08777 A
I2 = Δ2/Δ = −1200/4512 = −0.266 A
I3 = Δ3/Δ = −13776/4512 = −3.053 A
Answer
IR5 = I2 − I3 = 2.787 A
VR5 = IR5·R5 = 2.787·2 = 5.574 V
A negative mesh current flows anticlockwise.
7.Superposition
Answer: PR3 = 6.773 W
Superposition: in a linear circuit, any voltage or current is the sum of the responses to each independent source acting alone. To switch a source off, replace an ideal voltage source with a short circuit and an ideal current source with an open circuit. Resistors stay where they are.
Case 1 · V1 acting alone
Iₛ becomes an open circuit, so R₃ and R₄ form one series branch from A to ground, in parallel with R₂.
R3+R4 = 6+20 = 26 Ω
R2 ∥ (R3+R4) = 12·26/(12+26) = 8.211 Ω
VA = 12·8.211/(12+8.211) = 4.875 V
VB = VA·R4/(R3+R4) = 4.875·20/26 = 3.75 V
IR3′ = (VA − VB)/R3 = (4.875 − 3.75)/6 = 0.1875 A
Case 2 · Is acting alone
V₁ becomes a short, so R₁ is in parallel with R₂. Iₛ splits at B between R₄ and the path through R₃.
R1 ∥ R2 = 12·12/(12+12) = 6 Ω
Req = R4 ∥ (R3+R1∥R2) = 20 ∥ 12 = 7.5 Ω
VB = Is·Req = 2·7.5 = 15 V
VA = VB·(R1∥R2)/(R3+R1∥R2) = 15·6/12 = 7.5 V
IR3″ = (VA − VB)/R3 = (7.5 − 15)/6 = −1.25 A
Add the current contributions
IR3 = IR3′ + IR3″ = 0.1875 + (−1.25) = −1.062 A
Power in the resistor
Power depends on the square of the current, so it does not obey superposition: add the currents first, then square.
PR3 = IR3²·R3 = (−1.062)²·6 = 6.773 W
Answer
PR3 = 6.773 W
Adding the powers of the separate cases would give 9.586 W, which is wrong.
8.Superposition
Answer: IR3 = −1.368 A
Superposition: in a linear circuit, any voltage or current is the sum of the responses to each independent source acting alone. To switch a source off, replace an ideal voltage source with a short circuit and an ideal current source with an open circuit. Resistors stay where they are.
Case 1 · V1 acting alone
V₂ becomes a short and Iₛ an open circuit. Seen from A, R₃ is in parallel with the series pair R₂+R₄.
R3 ∥ (R2+R4) = 2 ∥ 25 = 1.852 Ω
VA = 10·1.852/(6+1.852) = 2.358 V
VB = VA·R4/(R2+R4) = 2.358·15/25 = 1.415 V
IR3′ = (VA − 0)/R3 = (2.358 − 0)/2 = 1.179 A
Case 2 · Is acting alone
Both voltage sources become shorts. Iₛ splits at B between R₄ (now to ground) and R₂ in series with R₁ ∥ R₃.
R1 ∥ R3 = 1.5 Ω, so the left path is R2+1.5 = 11.5 Ω
Req = R4 ∥ 11.5 = 6.509 Ω
VB = Is·Req = (−5)·6.509 = −32.55 V
VA = VB·1.5/11.5 = −4.245 V
IR3″ = (VA − 0)/R3 = (−4.245 − 0)/2 = −2.123 A
Case 3 · V2 acting alone
V₁ becomes a short and Iₛ an open circuit. R₁ ∥ R₃ hangs from A, in series with R₂ back to B.
R1 ∥ R3 = 6·2/(6+2) = 1.5 Ω
VB = V2·(R2+R1∥R3)/(R4+R2+R1∥R3) = (−15)·11.5/26.5 = −6.509 V
VA = VB·(R1∥R3)/(R2+R1∥R3) = −6.509·1.5/11.5 = −0.8491 V
IR3‴ = (VA − 0)/R3 = (−0.8491 − 0)/2 = −0.4245 A
Add the contributions
IR3 = IR3′ + IR3″ + IR3‴
IR3 = 1.179 + (−2.123) + (−0.4245) = −1.368 A
A negative result means the real current flows against the arrow.
9.Thévenin & Norton
Answer: Rth = 6.714 Ω
Thévenin’s theorem: any linear two-terminal network behaves like a single voltage source Vth in series with a resistance Rth. Norton’s theorem gives the same network as a current source IN = Vth/Rth in parallel with Rth.
Find Rth with every source switched off
Replace voltage sources with shorts and current sources with opens, then look into the circuit from a–b.
R1 ∥ R2 = 12·2/(12+2) = 1.714 Ω
Rth = (R1 ∥ R2) + R3 = 1.714 + 5 = 6.714 Ω
10.Thévenin & Norton
Answer: IN = 7 A
Thévenin’s theorem: any linear two-terminal network behaves like a single voltage source Vth in series with a resistance Rth. Norton’s theorem gives the same network as a current source IN = Vth/Rth in parallel with Rth.
Find Rth with every source switched off
Replace voltage sources with shorts and current sources with opens, then look into the circuit from a–b.
R1 ∥ R2 = 2·6/(2+6) = 1.5 Ω
Rth = (R1 ∥ R2) + R3 = 1.5 + 3 = 4.5 Ω
Find Vth, the open-circuit voltage
With a–b open, the only path for Iₛ is through R₃ into node A. Find V_A by superposition of V₁ and Iₛ, then add the drop across R₃.
VA = V1·R2/(R1+R2) + Is·(R1∥R2) = 13.5 + 4·1.5 = 19.5 V
Vth = VB = VA + Is·R3 = 19.5 + 4·3 = 31.5 V
Norton equivalent
A Norton source is the same circuit seen as a current source in parallel with R_th. Its current is the short-circuit current at a–b.
IN = Vth/Rth = 31.5/4.5 = 7 A
11.RC & RL transients
Answer: t = 16.09 ms
First-order transients: in a circuit with one capacitor or one inductor, every voltage and current moves exponentially from its initial value to its final value: x(t) = x(∞) + [x(0) − x(∞)]·e−t/τ, with τ = RC or τ = L/R. After about 5τ the circuit has settled.
Time constant
τ = L/R = 150 mH / 15 Ω = 10 ms
Solve for the time
0.4 = 2·e−t/τ → t = τ·ln(2/0.4)
t = 10·ln(5) = 16.09 ms
Answer
t = 16.09 ms
12.RC & RL transients
Answer: i = 0.9459 A
First-order transients: in a circuit with one capacitor or one inductor, every voltage and current moves exponentially from its initial value to its final value: x(t) = x(∞) + [x(0) − x(∞)]·e−t/τ, with τ = RC or τ = L/R. After about 5τ the circuit has settled.
Initial value, final value, time constant
Before t = 0 both resistors are in the loop; afterwards the closed switch bypasses R₂.
i(0) = 20/(20 + 10) = 0.6667 A
i(∞) = 20/20 = 1 A
τ = L/R = 220/20 = 11 ms
i(t) = 1 + (0.6667 − 1)·e−t/τ
Current at the given time
i(20) = 1 + (−0.3333)·e−20/11 = 0.9459 A
Answer
i = 0.9459 A
13.AC impedance & phasors
Answer: I = 0.5637 A
AC circuits with phasors: resistors, inductors and capacitors have impedances R, jωL and 1/(jωC), with ω = 2πf. In series, impedances add like resistances, but as complex numbers. Rms current and voltage follow Ohm’s law with |Z|.
Reactances
ω = 2πf = 2π·60 = 377 rad/s
XL = ωL = 377·0.05 = 18.85 Ω
XC = 1/(ωC) = 1/(377·47·10⁻⁶) = 56.44 Ω
Impedance
In series the impedances add as complex numbers: Z = R + j(XL − XC).
The same current flows through every element of a series circuit.
I = V/|Z| = 24/42.58 = 0.5637 A
Answer
I = 0.5637 A
14.AC impedance & phasors
Answer: I = 4.086 A
AC circuits with phasors: resistors, inductors and capacitors have impedances R, jωL and 1/(jωC), with ω = 2πf. In series, impedances add like resistances, but as complex numbers. Rms current and voltage follow Ohm’s law with |Z|.
Reactance
XC = 1/(2π·60·100·10⁻⁶) = 26.53 Ω
Parallel combination
Multiply top and bottom by the complex conjugate to split Zp into real and imaginary parts.
AC power: apparent power S = V·I (VA) splits into real power P = S·cos φ (W), which does useful work, and reactive power Q = S·sin φ (var), which moves back and forth between source and load. The power factor is cos φ. A capacitor in parallel supplies reactive power locally, so the line current drops for the same real power.
Current
|Z| = √(12² + 9²) = 15 Ω
I = V/|Z| = 120/15 = 8 A
Reactive power
Q = I²·X = 8²·9 = 576 var
Answer
Q = 576 var
16.AC power & power factor
Answer: I = 145.9 A
AC power: apparent power S = V·I (VA) splits into real power P = S·cos φ (W), which does useful work, and reactive power Q = S·sin φ (var), which moves back and forth between source and load. The power factor is cos φ. A capacitor in parallel supplies reactive power locally, so the line current drops for the same real power.
Reactive power before and after
The real power P does not change; only the reactive power drawn from the supply does.
Q1 = 29·tan(arccos 0.75) = 25.58 kvar
QC = V²·2πf·C = 240²·2π·50·330·10⁻⁶ = 5972 var = 5.972 kvar
Q2 = 25.58 − 5.972 = 19.6 kvar
New apparent power
S2 = √(29² + 19.6²) = 35 kVA
New line current
I = S2/V = 35005/240 = 145.9 A
Answer
I = 145.9 A
17.Three-phase power
Answer: IL = 59.71 A
Balanced three-phase systems: in a Y (star) connection the line-to-line voltage is √3 times the phase voltage, VL = √3·Vph, and the line current equals the phase current. In a Δ (delta) connection the line-to-line voltage equals the phase voltage and the line current is √3 times the phase current, IL = √3·Iph. The total power is three times the power of one phase: P = 3·Vph·Iph·cos φ = √3·VL·IL·cos φ.
Electrical input power
Pin = Pout/η = 55/0.94 = 58.51 kW
Line current
IL = Pin/(√3·VL·cos φ) = 58511/(√3·690·0.82) = 59.71 A
Answer
IL = 59.71 A
18.Three-phase power
Answer: QC = 203.7 kvar
Balanced three-phase systems: in a Y (star) connection the line-to-line voltage is √3 times the phase voltage, VL = √3·Vph, and the line current equals the phase current. In a Δ (delta) connection the line-to-line voltage equals the phase voltage and the line current is √3 times the phase current, IL = √3·Iph. The total power is three times the power of one phase: P = 3·Vph·Iph·cos φ = √3·VL·IL·cos φ. Power factor correction: capacitors supply reactive power locally, QC = P·(tan φ1 − tan φ2). Each of the three capacitors supplies QC/3 = V²·ω·C, where V is the voltage across that capacitor: VL in a Δ bank, VL/√3 in a Y bank.
Reactive power before and after
The real power is unchanged, so each power factor fixes the reactive power: Q = P·tan φ.
Q1 = 300·tan(acos 0.75) = 300·0.8819 = 264.6 kvar
Q2 = 300·tan(acos 0.98) = 300·0.2031 = 60.92 kvar
Reactive power from the capacitors
QC = Q1 − Q2 = 203.7 kvar
Answer
QC = 203.7 kvar
19.Transformers
Answer: R1′ = 576 Ω
Ideal transformer: the voltages are in the ratio of the turns and the currents in the inverse ratio: V₁/V₂ = N₁/N₂ = a and I₁/I₂ = N₂/N₁ = 1/a, so the power in equals the power out, V₁·I₁ = V₂·I₂. A load impedance Z on the secondary looks like a²·Z from the primary.
Referred resistance
The voltage goes up by a and the current down by a, so the ratio V/I goes up by a².
R1′ = a²·RL = 12²·4 = 576 Ω
Answer
R1′ = 576 Ω
20.Transformers
Answer: Pcu,fl = 817.9 W
Transformer losses: the core loss (hysteresis and eddy currents) depends on the voltage and is the same at any load. The copper loss in the windings goes with the current squared, so at a fraction x of rated load it is x²·Pcu,fl. Efficiency η = Pout/(Pout + Pcore + Pcu), with Pout = x·S·pf. The efficiency is highest at the load where the copper loss equals the core loss.
Output and input power
Pout = 50·0.95 = 47.5 kW
Pin = 47500/0.975 = 48718 W
Total and copper losses
Ploss = 48718 − 47500 = 1218 W
Pcu,fl = 1218 − 400 = 817.9 W
Answer
Pcu,fl = 817.9 W
21.Op-amp circuits
Answer: Rf = 235 kΩ
Ideal op-amp rules: with negative feedback, the op-amp drives its output so that its two inputs sit at the same voltage (V₋ = V₊), and no current flows into either input. Writing KCL at the inverting input with these two facts gives the output.
Gain of a non-inverting amplifier
V₋ = V₊ = Vin, and the current through R₁ also flows through Rf, so Vout = Vin·(1 + Rf/R₁).
Av = 1 + Rf/R1
Rf = (51 − 1)·4.7 = 235 kΩ
Answer
Rf = 235 kΩ
22.Op-amp circuits
Answer: Vout = −2.01 V
Ideal op-amp rules: with negative feedback, the op-amp drives its output so that its two inputs sit at the same voltage (V₋ = V₊), and no current flows into either input. Writing KCL at the inverting input with these two facts gives the output.
Gain of each stage
A1 = −Rf1/R1 = −4.7/1 = −4.7
A2 = 1 + Rf2/R2 = 1 + 2/4.7 = 1.426
Stage by stage
V1 = −4.7·0.3 = −1.41 V
Vout = 1.426·(−1.41) = −2.01 V
Answer
Vout = −2.01 V
23.Diodes & transistors
Answer: IZ = 17.43 mA
Zener regulator: a reverse-biased Zener diode holds its voltage VZ while its current stays above a minimum IZ,min. The series resistor R takes the difference between input and output: IR = (Vin − VZ)/R. That current splits between the load, IL = VZ/RL, and the Zener: IZ = IR − IL. Design for the worst cases: the lowest input with the largest load must still leave IZ,min, and the highest input with no load gives the largest Zener power PZ = VZ·IZ.
Resistor current
IR = 12.9/680 = 18.97 mA
Load current
IL = 5.1/3300 = 1.545 mA
Zener current
IZ = 18.97 − 1.545 = 17.43 mA
Answer
IZ = 17.43 mA
24.Diodes & transistors
Answer: PZ,max = 118.3 mW
Zener regulator: a reverse-biased Zener diode holds its voltage VZ while its current stays above a minimum IZ,min. The series resistor R takes the difference between input and output: IR = (Vin − VZ)/R. That current splits between the load, IL = VZ/RL, and the Zener: IZ = IR − IL. Design for the worst cases: the lowest input with the largest load must still leave IZ,min, and the highest input with no load gives the largest Zener power PZ = VZ·IZ.
Worst-case Zener current
IZ = 10.9/470 = 23.19 mA
Zener power
PZ = 5.1·23.19 = 118.3 mW
Answer
PZ,max = 118.3 mW
25.Number systems
Answer: N = 121
Positional number systems: each digit is worth its value times a power of the base. In binary the places are worth 1, 2, 4, 8, 16, …; in hexadecimal 1, 16, 256, …, with A–F standing for 10–15. In 8-bit two's complement the leftmost bit is worth −128 instead of +128, which is how negative numbers are stored.
Add the place values
The other bits keep their normal positive values.
64 + 32 + 16 + 8 + 1 = 121
Answer
N = 121
26.Number systems
Answer: M = 3600 KiB
Positional number systems: each digit is worth its value times a power of the base. In binary the places are worth 1, 2, 4, 8, 16, …; in hexadecimal 1, 16, 256, …, with A–F standing for 10–15. In 8-bit two's complement the leftmost bit is worth −128 instead of +128, which is how negative numbers are stored.
Bits and bytes
1280·720·32 = 29491200 bit = 3686400 B
Convert to KiB
3686400/1024 = 3600 KiB
Answer
M = 3600 KiB
27.Digital logic: gates, K-maps & flip-flops
Answer: AB = 01, CD = 00
Karnaugh maps: the cells are ordered in Gray code (00, 01, 11, 10), so neighbouring cells, including the ones across the edges, differ in exactly one variable. Group the 1s in rectangles of 1, 2, 4, 8 or 16 cells, as large as possible and as few as possible, until every 1 is covered. Each group is one product term: the variables that stay constant inside it. A group of 2ᵏ cells loses k variables. Don't-cares (X) may be used to make groups bigger but never have to be covered. Grouping the 0s instead gives the minimal POS form.
Neighbours of each 1
A 1 with a neighbouring 1 can join a group of two or more.
m4: m5, m6, m0, m12 → 0
The isolated 1
m4 = A′BC′D′ → AB = 01, CD = 00
Answer
AB = 01, CD = 00
28.Digital logic: gates, K-maps & flip-flops
Answer: fout = 0.4 kHz
Flip-flops and counters: a flip-flop changes only at the active clock edge. D copies its input (Q⁺ = D); T toggles when T = 1; JK holds for 00, resets for 01, sets for 10 and toggles for 11. An n-bit binary counter has 2ⁿ states and counts modulo 2ⁿ; a mod-N counter goes 0, 1, …, N − 1 and back to 0, and needs the smallest n with 2ⁿ ≥ N flip-flops. Each stage of a ripple counter halves the frequency, so the last output of a mod-N counter runs at fclk/N. A Johnson counter of n flip-flops has 2n states, a ring counter n.
Frequency division
fout = 20 kHz / 50 = 0.4 kHz
Answer
fout = 0.4 kHz
29.Laplace transforms
Answer: f(0.3) = 0.8945
Laplace transform: F(s) = ∫₀∞ f(t)·e−st dt turns derivatives into multiplications by s: ℒ{f′} = sF(s) − f(0), ℒ{f″} = s²F(s) − s·f(0) − f′(0). Standard pairs: 1 ↔ 1/s, e−at ↔ 1/(s + a), t·e−at ↔ 1/(s + a)², sin ωt ↔ ω/(s² + ω²), cos ωt ↔ s/(s² + ω²), and a shift s → s + σ multiplies the time function by e−σt. To invert a rational F(s), split it into partial fractions: the residue of a simple pole p is A = [(s − p)·F(s)] at s = p. Final value theorem: f(∞) = lims→0 s·F(s), valid only when all poles of s·F(s) lie in the left half-plane. Initial value theorem: f(0⁺) = lims→∞ s·F(s).
Factor the denominator
s² + 6s + 9 = (s + 3)²
Partial fractions
4s + 6 = 4(s + 3) + −6
F(s) = 4/(s + 3) − 6/(s + 3)²
Inverse transform
f(t) = 4·e−3t − 6·t·e−3t
f(0.3) = (4 − 6·0.3)·e−3·0.3 = 0.8945
Answer
f(0.3) = 0.8945
30.Laplace transforms
Answer: g(0.5) = 1.569
Laplace transform: F(s) = ∫₀∞ f(t)·e−st dt turns derivatives into multiplications by s: ℒ{f′} = sF(s) − f(0), ℒ{f″} = s²F(s) − s·f(0) − f′(0). Standard pairs: 1 ↔ 1/s, e−at ↔ 1/(s + a), t·e−at ↔ 1/(s + a)², sin ωt ↔ ω/(s² + ω²), cos ωt ↔ s/(s² + ω²), and a shift s → s + σ multiplies the time function by e−σt. To invert a rational F(s), split it into partial fractions: the residue of a simple pole p is A = [(s − p)·F(s)] at s = p. Final value theorem: f(∞) = lims→0 s·F(s), valid only when all poles of s·F(s) lie in the left half-plane. Initial value theorem: f(0⁺) = lims→∞ s·F(s).
Transfer function
G(s) = Y(s)/U(s) = (3s + 16)/(s² + 6s + 8)
Partial fractions
s² + 6s + 8 = (s + 2)(s + 4)
A = 5, B = −2
Impulse response
g(t) = 5·e−2t − 2·e−4t
g(0.5) = 1.569
Answer
g(0.5) = 1.569
31.Block diagrams
Answer: css = 14.29
Block-diagram algebra: blocks in series multiply (G₁·G₂), blocks in parallel add (G₁ + G₂), and a loop with forward path G and feedback path H reduces to T = G/(1 + G·H) for negative feedback and G/(1 − G·H) for positive feedback. Reduce inner loops first, then work outwards. The closed-loop poles are the roots of the characteristic equation 1 + G(s)H(s) = 0. For a stable loop, a step input of size A gives the steady-state output A·T(0); with unity feedback the steady-state error to a step is A/(1 + Kp) with Kp = G(0).
Block-diagram algebra: blocks in series multiply (G₁·G₂), blocks in parallel add (G₁ + G₂), and a loop with forward path G and feedback path H reduces to T = G/(1 + G·H) for negative feedback and G/(1 − G·H) for positive feedback. Reduce inner loops first, then work outwards. The closed-loop poles are the roots of the characteristic equation 1 + G(s)H(s) = 0. For a stable loop, a step input of size A gives the steady-state output A·T(0); with unity feedback the steady-state error to a step is A/(1 + Kp) with Kp = G(0).
Characteristic equation
s³ + 8s² + 12s + K = 0
Routh array
s³ | 1 12
s² | 8 K
s¹ | (8·12 − K)/8
s⁰ | K
Stability limit
All entries of the first column must be positive.
Kmax = 8·12 = 96
Frequency of oscillation
8·(jω)² + 96 = 0 → ω² = 96/8 = 12
ω = 3.464 rad/s
Answer
ω = 3.464 rad/s
33.Step response
Answer: ts = 1.143 s
Step response: a first-order system G(s) = K/(τs + 1) answers a step of size U with y(t) = K·U·(1 − e−t/τ): it reaches 63.2 % of the final value K·U after one time constant τ and 98 % after 4τ. A second-order system G(s) = K·ωₙ²/(s² + 2ζωₙs + ωₙ²) has the poles s = −ζωₙ ± jωd with ωd = ωₙ√(1 − ζ²). For 0 < ζ < 1 the step response overshoots: percent overshoot %OS = 100·e−ζπ/√(1−ζ²), peak time tp = π/ωd, and the 2 % settling time ts ≈ 4/(ζωₙ). Compare the denominator with s² + 2ζωₙs + ωₙ² to read off ωₙ and ζ. For a mass–spring–damper ωₙ = √(k/m) and ζ = c/(2√(km)); for a series RLC circuit ωₙ = 1/√(LC) and ζ = (R/2)·√(C/L).
Compare with the standard form
The denominator must match s² + 2ζωₙs + ωₙ².
ωₙ² = 30 → ωₙ = 5.477 rad/s
2ζωₙ = 7 → ζ = 7/(2·5.477) = 0.639
Result
ζωₙ = 3.5 → ts ≈ 4/3.5 = 1.143 s
Answer
ts = 1.143 s
34.Step response
Answer: K = 17.88
Step response: a first-order system G(s) = K/(τs + 1) answers a step of size U with y(t) = K·U·(1 − e−t/τ): it reaches 63.2 % of the final value K·U after one time constant τ and 98 % after 4τ. A second-order system G(s) = K·ωₙ²/(s² + 2ζωₙs + ωₙ²) has the poles s = −ζωₙ ± jωd with ωd = ωₙ√(1 − ζ²). For 0 < ζ < 1 the step response overshoots: percent overshoot %OS = 100·e−ζπ/√(1−ζ²), peak time tp = π/ωd, and the 2 % settling time ts ≈ 4/(ζωₙ). Compare the denominator with s² + 2ζωₙs + ωₙ² to read off ωₙ and ζ. For a mass–spring–damper ωₙ = √(k/m) and ζ = c/(2√(km)); for a series RLC circuit ωₙ = 1/√(LC) and ζ = (R/2)·√(C/L).
Closed-loop transfer function
T(s) = K/(s² + 5s + K)
Damping ratio from the overshoot
ζ = −ln(0.1)/√(π² + ln²(0.1)) = 0.5912
Gain
ωₙ = 5/(2ζ) = 4.229 rad/s
K = ωₙ² = 17.88
Answer
K = 17.88
35.Bode plots & margins
Answer: φ = 63.31 °
Frequency response: substitute s = jω in the transfer function. The magnitude in decibels is 20·log₁₀|H(jω)| and the phase is the sum of the angles of the numerator factors minus those of the denominator factors. A first-order RC or RL filter has its corner (−3 dB) frequency at ωc = 1/(RC) or R/L, and fc = ωc/(2π); a low-pass filter gives |H| = 1/√(1 + (ω/ωc)²) and φ = −atan(ω/ωc). In the asymptotic (straight-line) Bode plot each pole bends the magnitude down by 20 dB/decade at its corner frequency, each zero bends it up by 20 dB/decade, and an integrator 1/s gives −20 dB/decade at all frequencies. Gain crossover ωc: |L(jω)| = 1 (0 dB); phase margin PM = 180° + ∠L(jωc). Phase crossover ω180: ∠L(jω) = −180°; gain margin GM = −20·log₁₀|L(jω180)| dB. The closed loop is stable when both margins are positive.
Corner frequency
ωc = R/L = 10/0.1 = 100 rad/s
fc = 15.92 Hz → f/fc = 8/15.92 = 0.5027
Phase
φ = 90° − atan(0.5027) = 63.31°
Answer
φ = 63.31°
36.Bode plots & margins
Answer: ωc = 2.244 rad/s
Frequency response: substitute s = jω in the transfer function. The magnitude in decibels is 20·log₁₀|H(jω)| and the phase is the sum of the angles of the numerator factors minus those of the denominator factors. A first-order RC or RL filter has its corner (−3 dB) frequency at ωc = 1/(RC) or R/L, and fc = ωc/(2π); a low-pass filter gives |H| = 1/√(1 + (ω/ωc)²) and φ = −atan(ω/ωc). In the asymptotic (straight-line) Bode plot each pole bends the magnitude down by 20 dB/decade at its corner frequency, each zero bends it up by 20 dB/decade, and an integrator 1/s gives −20 dB/decade at all frequencies. Gain crossover ωc: |L(jω)| = 1 (0 dB); phase margin PM = 180° + ∠L(jωc). Phase crossover ω180: ∠L(jω) = −180°; gain margin GM = −20·log₁₀|L(jω180)| dB. The closed loop is stable when both margins are positive.
Gain crossover
ω⁴ + 100ω² − 529 = 0
ω² = (−100 + √(10000 + 4·529))/2 = 5.036
ωc = 2.244 rad/s
Answer
ωc = 2.244 rad/s
37.Stability: Routh–Hurwitz & root locus
Answer: N = 2
Routh–Hurwitz criterion: a linear system is stable when every root of its characteristic polynomial lies in the left half of the s-plane. Write the coefficients alternately into the first two rows of the Routh array. Each entry of a new row comes from the two rows above it; for a cubic a₃s³ + a₂s² + a₁s + a₀ the s¹ entry is b₁ = (a₂·a₁ − a₃·a₀)/a₂. The number of sign changes in the first column equals the number of roots in the right half-plane. With a gain K in the coefficients, every first-column entry must stay positive: the gain that makes the s¹ entry zero is the stability limit, and the s² row then gives the frequency of the sustained oscillation.
Characteristic polynomial
s³ + 5s² + 4s + 40 = 0
Routh array
s³: 1, 4
s²: 5, 40
s¹: −4
s⁰: 40
Sign changes in the first column
1 → 5 → −4 → 40
N = 2
Answer
N = 2
The gain is above the limit K = 20, so a complex pair has crossed into the right half-plane.
38.Stability: Routh–Hurwitz & root locus
Answer: σa = −2.5
Root locus: as the gain K goes from 0 to ∞, the closed-loop poles, the roots of 1 + K·G(s) = 0, move from the open-loop poles to the open-loop zeros or to infinity. A point on the real axis belongs to the locus when the number of real poles and zeros to its right is odd. The n − m branches that go to infinity follow asymptotes at the angles (2q + 1)·180°/(n − m), which start from the centroid σₐ = (Σ poles − Σ zeros)/(n − m). Branches leave or join the real axis where dK/ds = 0. The angle condition ∠G(s) = 180° fixes the shape, and the magnitude condition K = 1/|G(s)| gives the gain at any point of the locus.
Poles and zeros
poles: 0, −2, −6
zeros: −3
n − m = 3 − 1 = 2
Centroid
σa = (−8 − (−3))/2 = −2.5
Answer
σa = −2.5
The 2 asymptotes leave the centroid at angles of 90°, 270°.
39.Steady-state error & PID control
Answer: ess = 12.5
Steady-state error: in a unity-feedback loop with open-loop transfer function G(s) the error is E(s) = R(s)/(1 + G(s)), and by the final value theorem ess = lims→0 s·E(s). The system type is the number of poles of G(s) at s = 0. The error constants are Kp = lim G(s), Kv = lim s·G(s) and Ka = lim s²·G(s), all for s → 0. A step of size A gives ess = A/(1 + Kp), a ramp A·t gives A/Kv and a parabola A·t²/2 gives A/Ka. A type-0 loop follows a step with a finite error, a type-1 loop follows it exactly and a ramp with a finite error.
Velocity constant
Kv = lim s·G(s) = 0.04
Ramp error
ess = 0.5/0.04 = 12.5
Answer
ess = 12.5
40.Steady-state error & PID control
Answer: ts = 4 s
P, PI and PID control: the controller C(s) = Kp + Ki/s + Kd·s acts on the error. A proportional gain makes the loop faster and reduces the error of a type-0 plant, but never removes it. The integral term adds a pole at s = 0: the system type rises by one, and a step is followed without error. The derivative term adds damping. To choose gains, write the closed-loop characteristic polynomial and compare it with s² + 2ζωns + ωn². Then %OS = 100·e−ζπ/√(1−ζ²), tp = π/ωd with ωd = ωn√(1 − ζ²), and ts ≈ 4/(ζωn).
Characteristic polynomial
s(s + 2) + 2·4 = s² + 2s + 8
ωₙ and ζ
ωₙ = √8 = 2.828 rad/s
ζ = 2/(2·2.828) = 0.3536
Settling time
ζωₙ = 2/2 = 1
ts ≈ 4/1 = 4 s
Answer
ts = 4 s
The settling time does not depend on K here: raising K only makes the response oscillate faster.
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